Semi-analytical study of free vibration of composite shells of revolution based on the Reissner-Mindlin assumption

International Journal of Solids and Structures

Volumn 33, Issue 6, 1996, Pages 851-863

  Xi, Z C ^a   Yam, L H ^a   Leung, T P ^a  

^a HONG KONG POLYTECHNIC UNIVERSITY   (Hong Kong)

Author keywords

[No Author keywords available]

Indexed keywords

COMPOSITE STRUCTURES; ELASTIC MODULI; LAMINATED COMPOSITES; NATURAL FREQUENCIES; NUMERICAL METHODS; SHEAR DEFORMATION; STIFFNESS; STRAIN; STRUCTURAL ANALYSIS; VIBRATIONS (MECHANICAL);

CIRCUMFERENTIAL WAVE NUMBER; COMPOSITE SHELLS; FREE VIBRATION; PLY ANGLE; REISSNER-MINDLIN ASSUMPTION; SEMI-ANALYTICAL STUDY; STACKING SEQUENCE; TRANSVERSE SHEAR DEFORMATION;

SHELLS (STRUCTURES);

EID: 0030107331     PISSN: 00207683     EISSN: None     Source Type: Journal    
DOI: 10.1016/0020-7683(95)00063-G     Document Type: Article

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